CN205936069U - Aircraft hinge subassembly - Google Patents
Aircraft hinge subassembly Download PDFInfo
- Publication number
- CN205936069U CN205936069U CN201620881296.7U CN201620881296U CN205936069U CN 205936069 U CN205936069 U CN 205936069U CN 201620881296 U CN201620881296 U CN 201620881296U CN 205936069 U CN205936069 U CN 205936069U
- Authority
- CN
- China
- Prior art keywords
- poker
- hinge
- aircraft
- half hinge
- rear spar
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Tires In General (AREA)
Abstract
The utility model provides an aircraft hinge subassembly, including a left side narrow the page or leaf (1), the right side narrow the page or leaf (2), poker (3), a left side narrows page (1) and the right side narrows through poker (3) hinged joint between the page or leaf (2), aircraft hinge subassembly is arranged in connecting rudder face roof beam (5) and wing back beam (6) of aircraft, wherein, a left side narrow the page or leaf (1) link firmly on rudder face roof beam (5), the right side narrow the page or leaf (2) link firmly on wing back beam (6), left side page or leaf (1) and the right side page or leaf (2) that narrows that narrows is stretched out to poker (3) one end, and fix the one end that poker (3) stretches out on wing back beam (6) through fastener (4). The utility model provides an aircraft hinge subassembly can restrict the poker drunkenness, connects reliably to easily installation and dismantlement.
Description
Technical field
The utility model belongs to airplane structural parts field, is related to aircraft hinge assembly.
Background technology
In aeroplane structure design a lot of positions commonly used to hinge, the maintenance lid such as in wing-box, flaperon, liter
The trimmer of fall rudder, auxiliary intake valve of air intake duct etc., and the installation of hinge and fastening often occur a lot of problems.As Fig. 1
With the hinge shown in Fig. 2, using for present aircraft wing leading edge lid, this hinge is made up of two halves, and centre is carried out by poker
Connect.In order to poker is unlikely to deviate from hinge hole, bending process are carried out to the two ends of poker.The shortcoming of this hinge is poker edge
Open up to easy play, easily poker is caused to damage during installation and removal extremely inconvenience, and installation and removal.
Utility model content
The purpose of this utility model is to provide a kind of aircraft hinge assembly, solves the problems, such as poker play.
The purpose of this utility model is achieved through the following technical solutions：A kind of aircraft hinge assembly, including left half hinge, the right side
Half hinge, poker, pass through described poker chain connection, described aircraft hinge group between described left half hinge and described right half hinge
Part is used for connecting rudder face beam and the wing rear spar in aircraft, and wherein, described left half hinge is connected on described rudder face beam, the described right side
Half hinge is connected on described wing rear spar, and described left half hinge and described right half hinge are stretched out in described poker one end, and pass through
One end that described poker stretches out is fixed on described wing rear spar securing member.
Preferably, one end that described poker stretches out is bent into an annular section, and this described annular section is arranged in institute
State on right half hinge.
Preferably, described securing member includes bolt, two packing rings and slotted nut, and two described packing rings are arranged in
Near described right half hinge side and opposite side, it is described logical that described bolt runs through connection through described packing ring to described wing rear spar
Annular section in bar and described wing rear spar, and fixed by screwing described slotted nut.
Preferably, described securing member also includes split pin, and described split pin passes through described slotted nut and described bolt
Both fixing, prevent described slotted nut from getting loose.
The having the beneficial effects that of a kind of aircraft hinge assembly provided by the utility model, hinge assembly is simple and practical, even
Connect reliability, install and easy accessibility, and poker is difficult play, serviceability is good, and maintenance cost is low.
Brief description
Fig. 1 is the aircraft hinge assembly schematic diagram of prior art；
Fig. 2 is the aircraft hinge assembly profile of prior art；
Fig. 3 is aircraft hinge assembly structural representation of the present utility model.
Reference：
A 1- left side half hinge, the 2- right side half hinge, 3- poker, 4- securing member, 5- rudder face beam, 6- wing rear spar, 31- ring part
Point, 41- bolt, 42- packing ring, 43- slotted nut, 44- split pin.
Specific embodiment
For making purpose, technical scheme and advantage that the utility model is implemented clearer, below in conjunction with the utility model
Accompanying drawing in embodiment, is further described in more detail to the technical scheme in the utility model embodiment.In the accompanying drawings, ad initio
To the element that same or similar label represents same or similar element or has same or like function eventually.Described reality
Applying example is a part of embodiment of the present invention, rather than whole embodiments.Embodiment below with reference to Description of Drawings is to show
Example property it is intended to be used for explaining the utility model, and it is not intended that to restriction of the present utility model.Based in the utility model
Embodiment, the every other embodiment that those of ordinary skill in the art are obtained under the premise of not making creative work,
Broadly fall into the scope of the utility model protection.
Below in conjunction with the accompanying drawings the utility model aircraft hinge assembly is described in further details.
A kind of aircraft hinge assembly, for connecting the rudder face beam 5 in aircraft and wing rear spar 6, this aircraft hinge assembly bag
Include left half hinge 1, right half hinge 2, poker 3, between left half hinge 1 and right half hinge 2, pass through poker 3 chain connection, constitute one
Individual hinge structure, wherein, left half hinge 1 is fixedly connected on rudder face beam 5 by rivet, and right half hinge 2 is fixed also by rivet
It is connected on wing rear spar 6, left half hinge 1 and right half hinge 2 are stretched out in this poker 3 one end, and are stretched poker 3 by securing member 4
The one end going out is fixed on wing rear spar 6, and one end that this poker 3 stretches out preferably is bent into the annular section 31 of a closure, ring
Form a hollow region in the middle of shape part 31, as shown in Figure 3, this annular section 31 is arranged in the right side half on wing rear spar 6
On hinge 2.This securing member 4 preferred bolt assembly, including 41, two packing rings 42 of bolt and slotted nut 43.Bolt assembly is fixed
The installation method of the poker 3 stretching out is as follows：First two packing rings 42 are arranged in wing rear spar 6 near right half hinge 2 side
And opposite side, that is, in Fig. 3 wing rear spar 6 both sides up and down, then by the screw portion in bolt 41 pass through wing rear spar 6 on the upside of
Packing ring 42, then run through hollow region and the wing rear spar 6 that the annular section 31 connecting in poker 3 is formed, be then then passed through
The packing ring 42 of wing rear spar 6 downside, finally screws slotted nut 43 and fixes this bolt 41, thus ensureing firmly installing of poker 3.
This securing member 4 can also add split pin 44, has pin-and-hole away from screw cap end in bolt 41 screw portion, and this pin-and-hole is along spiral shell
Bolt 41 radial direction is arranged, and slotted nut 43 is also equipped with pin-and-hole, and split pin 44 passes through pin-and-hole and spiral shell on slotted nut 43
Both pin-and-hole on bolt 41 is fixing, preventing slotted nut 43 from getting loose, also functioning to the effect of fixing poker 3, thus preventing from leading to simultaneously
Bar 3 play.
The above, specific embodiment only of the present utility model, but protection domain of the present utility model does not limit to
In this, any those familiar with the art in the technical scope that the utility model discloses, the change that can readily occur in
Change or replace, all should cover within protection domain of the present utility model.Therefore, protection domain of the present utility model should be with described
Scope of the claims is defined.
Claims (4)
1. a kind of aircraft hinge assembly, including left half hinge (1), right half hinge (2), poker (3), described left half hinge (1) with
Pass through described poker (3) chain connection, described aircraft hinge assembly is used for connecting the rudder in aircraft between described right half hinge (2)
Face beam (5) and wing rear spar (6), wherein, described left half hinge (1) is connected on described rudder face beam (5), described right half hinge
(2) it is connected in described wing rear spar (6) above it is characterised in that described left half hinge (1) and institute are stretched out in described poker (3) one end
State right half hinge (2), and by securing member (4), one end that described poker (3) stretches out is fixed on described wing rear spar (6).
2. aircraft hinge assembly according to claim 1 is it is characterised in that one end that described poker (3) stretches out is bent into
One annular section (31), described annular section (31) is arranged on described right half hinge (2).
3. aircraft hinge assembly according to claim 2 it is characterised in that described securing member (4) include bolt (41), two
Individual packing ring (42) and slotted nut (43), two described packing rings (42) are arranged in described wing rear spar (6) near the described right side
Half hinge (2) side and opposite side, described bolt (41) runs through, through described packing ring (42), the ring connecting in described poker (3)
Shape part (31) and described wing rear spar (6), and fixing by screwing described slotted nut (43).
4. aircraft hinge assembly according to claim 3 is it is characterised in that described securing member (4) also includes split pin
(44), described split pin (44) passes through described slotted nut (43) to fix both with described bolt (41), prevents described fluting spiral shell
Female (43) get loose.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620881296.7U CN205936069U (en) | 2016-08-15 | 2016-08-15 | Aircraft hinge subassembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620881296.7U CN205936069U (en) | 2016-08-15 | 2016-08-15 | Aircraft hinge subassembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205936069U true CN205936069U (en) | 2017-02-08 |
Family
ID=57920265
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620881296.7U Active CN205936069U (en) | 2016-08-15 | 2016-08-15 | Aircraft hinge subassembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205936069U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114212273A (en) * | 2021-12-10 | 2022-03-22 | 江西昌河航空工业有限公司 | Installation positioning device for sectional type long-hinge repair of helicopter |
-
2016
- 2016-08-15 CN CN201620881296.7U patent/CN205936069U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114212273A (en) * | 2021-12-10 | 2022-03-22 | 江西昌河航空工业有限公司 | Installation positioning device for sectional type long-hinge repair of helicopter |
| CN114212273B (en) * | 2021-12-10 | 2023-05-26 | 江西昌河航空工业有限公司 | Installation positioning device for repairing sectional long hinge of helicopter |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US20170183081A1 (en) | Multi-Rotor Passenger-Carrying Aircraft with Foldable Aircraft Arm | |
| CN104108463A (en) | Winglet Attach Fitting And Method For Attaching A Split Winglet To A Wing | |
| CN205675228U (en) | Docking structure on spar flange for a kind of aerofoil covering | |
| CN205936069U (en) | Aircraft hinge subassembly | |
| GB2575841A (en) | Wing assembly with fluid pipe | |
| CN205574254U (en) | Foldable many rotor unmanned aerial vehicle | |
| CN208137718U (en) | A kind of dismountable fashioned iron door hinge of flange face positioning | |
| CN108609159A (en) | Wing, empennage and aircraft | |
| CN201394360Y (en) | Model airplane no-aileron headstock assembly | |
| CN205909397U (en) | Air -conditioning indoor unit | |
| CN205396518U (en) | Unmanned aerial vehicle's folding arm component | |
| CN204368408U (en) | For being fixedly connected with the mounting structure of model plane fuselage and wing | |
| CN217575583U (en) | Aircraft body component's coupling assembling and aircraft | |
| CN209079818U (en) | A kind of automobile and its licence plate decorative panel assembly | |
| CN208602688U (en) | A kind of detachable rudder face rotating shaft mechanism of unmanned plane | |
| US11884411B2 (en) | Aircraft engine pylon having a movable assembly of cowls | |
| CN205837167U (en) | A kind of composite integral tank Wing-Body Configurations attachment means | |
| CN211543873U (en) | Double-intersection-point flap slide rail trailing edge suspension joint | |
| CN208947583U (en) | Wing, empennage and aircraft | |
| CN206091579U (en) | Handle and door lock panel's connection structure | |
| CN208855859U (en) | A kind of folding locking structure for unmanned plane installation | |
| CN203713484U (en) | Movable air filter support assembly | |
| CN207782741U (en) | A kind of high-strength stable and easy-to-dismount photovoltaic plant maintenance pedal | |
| CN205737249U (en) | A kind of vehicle-mounted access ladder device | |
| CN107970621B (en) | Modular model airplane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |